Flow phenomena encountered in the vicinity of Mach 1 are discussed. The application of the supercritical wing to this flight regime are discussed. Research work and flight tests performed by various American companies are detailed. (Author)


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    Title :

    The Supercritical Wing


    Contributors:
    D. Seidl (author)

    Publication date :

    1972


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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